Cessna 175 A B

Number of Active Aircraft: 1082 Active- Map


Years Produced: 1958-62. The aircraft earned a reputation for unreliability. The geared engine was the cause of most of the complaints. The aircraft is an all metal airframe designed to be a higher powered version of the popular 172 of the era. The C model raised the gross weight up by 100 additional pounds. Over 2000 Skylarks were produced. It was powered by a geared Continental GO-300 engine.

Wikipedia Cessna 175 reference:

Fuel Cost ($):
General Stats:
Seat Capacity: 4
Empty Weight: 1325 lbs
Max Weight 2350 lbs
Useful Load: 1025 lbs
Engine Name Continental GO-300C
Engine Number 1
Horsepower 175 HP
Never Exceed Speed: 153 kts
Stall speed: 0 kts
Service Ceiling: 15900 ft
Max Fuel 43 Gal
Performance/Efficiency Metrics:
Cruise Speed(75%BHP): 122 kts
GPH (75% BHP): 10.5
MPG (75% BHP) 11.6
Range (75% BHP): 415 nm
Fuel Cost Per Seat Mile 0.13 $
Fuel Cost Per Hour 63 $
MPG per 1000 lbs of Payload 11.91
F-T (Speed^2/FuelBurn) 14.2 HP
F-T Payload 14.6 kts
MPH To HP: 7 kts
T/O Roll - T/O over 50 FT OBST 0 ft / 1340 ft

SA00024NY Installation of Airwolf remote mounted engine oil filter kit AFC-K007 on single or multi-engine fixed wing light aircraft incorporating Lycoming reciprocating engines of 450 horsepower or less. Amended 10/3/2012
SA00027WI Installation of flap and aileron gap seals. Issued 2/11/1993
SA00061LA Installation of JPI digital tachometer. Amended 1/12/1996
SA00066SE Fabrication of interchangeable float spreader bars. Amended 10/10/2000
SA00068SE (PAGE 1) Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1) Amended 10/20/2010
SA00079NY Installation of Airwolf remote mounted engine oil filter kit AFC-K008 on single and multi engine fixed wing light aircraft incorporating Teledyne Continental reciprocating engines of 450 horsepower or less. Amended 10/31/2012
SA00081NY Installation of Iceman Aviation Supplies Inc. Carburetor Ice Detector. Amended 5/15/2002
SA00161BO (1 OF 3) Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.  Amended 2/8/2005
SA00162SE Installation of telemetry antennas. Reissued 5/28/1997
SA00165BO Installation of Avidyne Corporation Datalink Coupler part number 700-00015-000 per Avidyne Corporation Master Document List Document No. AVACP-006 dtd 1/2/93 or later FAA-approved revisions. Issued 2/20/2003
SA00186AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/14/1994
SA00188AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-26A. Reissued 11/14/1994
SA00194AT Installation of Appalachian Accessories carbon steel brake discs that have the melonite surface treatment P/N AA-40. Reissued 11/14/1994
SA00194BO Installation of P/N 2042 Landing Gear Warning System for amphibian aircraft. Reissued 1/23/2009
SA00211AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00212AT Installation of carbon steel brake discs that have melonite surface treatment. Reissued 11/17/1994
SA00215NY Installation of CAVU Model AM100 AVMIX engine fuel/air mixture setting system. Amended 8/14/1995
SA00240AT Installation of a wing mounted camera pod. Approved for installation on serial number R172-0297 ONLY. Amended 1/17/2002
SA00243BO (2 OF 5) Installation of Centurion Consulting Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100) or without roll steering (p/n 0025-5200). Amended 7/21/2011
SA00269BO (1OF 3) Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ) Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1 and Avidyne Mounting Tray P/N 700-00034-000. Reissued 4/9/2010
SA00270WI Installation of fiberglass replacement wing tips. Amended 6/23/2000
SA00272WI Replacement of hydraulic system pressure switch. Reissued 11/8/2007
SA00281BO Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ) Sensor Systems Inc. Antenna P/N S67-1575-109 or equivalent and optional Avidyne Mounting Tray P/N 700-00165-000 Amended 4/24/2012
SA00290BO (PAGE 1 ) Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX Reissued 7/1/2010
SA00297NY Conversion of tricycle landing gear to tail dragger. Issued 4/4/1995
SA00402SE Installation of a remote spin-on oil filter adapter. (GC-1B w/Lycoming or Cont 360 engine installed) Amended 1/23/2007
SA00406WI Installation of replacement flap trailing edge bulbs. (R172K XP) Amended 9/9/1999
SA00419NY Installation of cockpit utility light. Reissued 12/31/2002
SA00432SE (PG 4) Installation of EGT 701 series fuel flow instrument. Amended 4/12/2013
SA00459WI Energy absorbing seat. Amended 1/28/1997
SA00461SE Install a Lycoming O-360 series engine and Hartzell McCauley or Sensenich propeller (See STC for specifications). Amended 10/24/2002
SA00465NY Installation of Meterological Measurement System Model A1MMS-10 with optional installation of Telemetry Module Model AIRDAT-9600. Amended 10/28/1998
SA00496SE Installation of Oregon Aircraft Design Engine Mount Heat Shields. Amended 12/20/2000
SA00648SE Fabrication of R.M.D. Aircraft Lighting Inc. wing-tip and landing light Kit No. 00190-C. Issued 11/30/1998
SA00671NY Installation of AIRDAT Telemetry module. Amended 10/28/1998
SA00674CH Installation of Wipaire 2100 amphibian/seaplane floats. Amended 8/24/2005
SA00678SE Installation of J. P. Instruments 8Jimline EGT-100 series primary instruments Issued 3/5/1999
SA00679SE Installation of interior fiberglass trim panels. Amended 5/2/2011
SA00680SE (3 OF 6 Installation of Electronics International model UBG-16 or UBG-16T bar graph engine analyzer.  Reissued 7/8/2005
SA00709CH Installation of replacement wing root vent described by Dwg Nos. 8-30-96-1& 8-30-96-2 no rev both dtd 8/30/96 or later FAA app rev. Issued 7/9/1997
SA00709LA Installation of control wheel. Includes provisions only for a push-to-talk (PTT) switch. Separate FAA approval of PTT switch is required. Reissued 5/14/2002
SA00709SE Installation of replacement control surface skin panels. Issued 6/28/1999
SA00726SE Installation of a Lycoming O-360-A1AD engine and Hartzell HC-C2YK-1BF/7666A-2 propeller. Issued 8/10/1999
SA00728SE  Installation of various models of the Continental IO360 Engine Amended 3/21/2013
SA00760SE Installation of glare shield. Reissued 5/20/2010
SA00780SE (PAGE 1) Installation of the True Lock Safety Retention Axle Lock Nut System in accordance with AML No. SA00780SE dated February 1 2001 or later FAA approved revision. Amended 5/11/2010
SA00795CH Installation of Baumann Model BF-2550 floats. Reissued 4/27/2005
SA00796SE Installation of vortex generators on the wings and tail surfaces of the above model aircraft Amended 5/27/2004
SA00812CH Replace Cessna Sun Visor assemblies with Aircraft Replacement Fabricated Components tinted Sun Visor Assemblies. Reissued 6/30/2006
SA00831SE Installation of vortex generators on wings and tail surfaces. Issued 8/4/2000
SA00834SE Installation of vortex generators on wings and tail surfaces. Issued 8/11/2000
SA00861SE Page 4 Installation of J.P. Instruments (JPI) fuel flow indicating system Amended 4/12/2013
SA00871SE Cockpit sunvisor installation. Amended 5/11/2010
SA00897CH Installation of Domed (Bubble) Window Amended 12/4/2013
SA00897WI Installation of Concorde Battery Corporation (VRSLA) Valve regulated sealed lead acid battery. Issued 8/11/2000
SA00900CH Installation of Wipaire Model 2350 Amphibian/Seaplane Floats and McCauley Model 1A200/WFA propeller. Amended 9/28/2011
SA00919SE : Installation of vacuum stall warning system as either the primary or as a secondary stall warning system in accordance with drawings and instructions listed in AML SA00919SE. );INSERT INTO stc_table VALUES (  Issued 5/24/2001
SA00954SE (1 OF 2) Installation of J.P. Instruments (JPI) Primary Temperature Indicating System in accordance with JPI Installation Manual for the EDM 711 Report 106P Revision B dated August 2 2001 or later FAA approved revision. Amended 8/11/2003
SA01015SE Installation of eligible Alaska Tire and Rubber Company TSO-C62d Tires as listed in Approved Model List SA01015SE dated November 7 2001 or later FAA approved revision. Amended 10/4/2012
SA01026SE (PAGE 2) Improved fuel gascolator assembly. Amended 12/19/2012
SA01032WI Installation of external aerodynamic Vortelator Kit on airplanes Amended 7/11/2008
SA01074WI Installation of McFarlane Aviation Flap Roller Assembly Service Kit MCSK100 on various Cessna single-engine aircraft. Cessna Service Bulletin SEB95-3 must be complied with before this STC is installed. Issued 4/22/2002
SA01085LA (PAGE 1) Installation of the VNS 1000 Voice Navigation System. Reissued 4/26/2010 0:00
SA01105WI-D (1 OF 2) Installation of Bendix/King KMD 550/850 Multi-Function Display System with Optional Traffic Terrain and Weather Sensors. This STC also is approved for some single-engine aircraft. See SA01105WI-D (2 of 2). Amended 5/31/2007
SA01107SE RMD Aircraft Lighting high intensity discharge wingtip light manufactured Amended 4/2/2003
SA01118WI Installation of the Concorde FLA or VRSLA RG series batteries in the Cessna Single Engine Airplanes listed on the attached FAA Approved Model List (AML) No. SA01118WI dated October 17 2001 Amended 11/30/2013
SA01120SE Installation of Door Steward. Amended 3/4/2010
SA01157LA Installation of Electronics International Model FP-5 or FP-5L fuel flow/fuel pressure instrument as a replacement instrument. Reissued 1/20/2005
SA01158WI (1 OF 2) Installation of Aero Enhancements UV250-1 Supplemental Instrument Panel Lightning System. Amended 3/29/2005
SA01204LA Installation of replacement wing tip fairing assembly. Issued 10/3/2001
SA01205WI-D (1 OF 2) Installation of the KMD 250 Multi-Function Display System with Optional Internal VFR GPS and Optional Traffic and Weather Sensors. );INSERT INTO stc_table VALUES (  Amended 11/20/2007
SA01229SE Page 1 Installation of CNX80 GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Amended 6/27/2007
SA01233SE Manufacture of Alaskan Bushwheel Inc. (ABI) tail wheel and fork assembly per ABI Document ABI-3200B Revision A dated April 28 2005 or later FAA approved revision.  Amended 5/22/2012
SA01240SE (2 OF 5) Installation of secondary voltage indication system Reissued 4/3/2006 0:00
SA01280CH Installation of Challenger Spin-On Oil Filters.(For Cessna 182 model s/n 67042 and up) (For Cessna 421C model s/n 1017 thru 1404) Issued 8/29/2000
SA01298SE Installation of interior trim parts. Reissued 5/20/2010
SA01323WI Installation of flap gap seal per Aircraft Development Co. Drawing List 114-1 stamped FAA approved with a date of April 27 2005 or later. Conformity data for Drawing List 114-1 is derived from Drawing List 114-1 Revision C and STC Issued 4/27/2005
SA01324WI Installation of aileron gap seal per Aircraft Development Co. Drawing List 115-1 stamped FAA approved Issued 4/27/2005
SA01330LA (PAGE 1) Installation of alternate avionics support assembly. Reissued 10/6/2010
SA01356SE  Installation of Instrument Panel and Y Issued 12/22/2003
SA01386NY Installation of Fibre Glass Reinforced Plastic Nacelle Fairing Trade Name Exhaust Fairing . Reissued 10/9/2002
SA01435SE Installation of J.P. Instruments (JPI) Primary Engine Data Management System Amended 9/17/2013
SA01436SE (1 OF 2) Cockpit sunvisor retrofit kit. Issued 8/2/2004
SA01473SE (2 OF 5) Installation of a GTX 32 (mode C) GTX 33 (mode S) or GTX 33D (mode S with diversity) Remote Transponde Amended 5/21/2008
SA01487SE-D (Page 1) Installation of a GDL 69 or GDL 69A XM Satellite Receiver Amended 5/4/2012
SA01560WI-D Installation of the Honeywell KFD 840 Primary Flight Display System. );INSERT INTO stc_table VALUES ( REQUIRED DATA: AML No. 159-08325-0002 Revision - dated 12-1-2009. Later FAA approved revisions to the above listed data are incorporated without further revision to this Supplemental Type Certificate. Amended 7/22/2010
SA01646SE Installation of vortex generators on wings horizontal and vertical tail surfaces. Issued 2/28/2006
SA01660SE Installation of interior fiberglass panels. Reissued 5/20/2010
SA01669CH Installation of Challenger Reusable Air Filter Amended 6/21/2012
SA01679CH Install BRS-172 parachute recovery system. Amended 8/29/2012
SA01692SE (Page 1 OF 2) Installation of a Garmin GMX 200 Multi-Function Display Reissued 10/3/2012
SA01695SE (1 OF 5) Installation of an antenna Amended 2/15/2007
SA01714WI (Page 1) Installation of a Garmin GTX 330/330D/33/33D with ADS-B Out functionality Issued 5/1/2013
SA01765SE Installation of Alaskan Bushwheel Inc (ABI) TSO-C26d wheels Part Number (P/N) ABI-1010. Amended 10/11/2012
SA01800SE (PG 1) Fabrication and installation of new or replacement of existing instrument panel lights dimmer control.  Reissued 12/1/2011
SA01815CH Installation of Baumann Model BF2550A floats. For models 172I through 172P a gross weight of 2350 lbs. at a center of gravity range of plus 39.5 inches to plus 45.5 inches is approved. For models R172K and R172K with STCs SA1436CE and SA1437CE the maximum gross weight is limited to 2550 lbs. at a center og gravity range of plus 39.5 inches to plus 45.5 inches. Reissued 1/10/2005
SA01834CH (1 OF 2) Installation of the High Intensity Discharge Light Assembly Kit. Amended 3/20/2009
SA01860NY (1 OF 3) Installation of Graphic Engine Monitors (GEM) Models GEM-610 and GEMINI 1200.  Amended 5/31/2006
SA01861SE (PAGE 1)  Fabrication and installation of Landing Light Controller Reissued 12/1/2011
SA01923LA Installation of the P-1000 Digital Electronic Tachometer. Issued 1/23/2007
SA01933LA-D Page 1 Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation );INSERT INTO stc_table VALUES ( System Amended 4/1/2013
SA01933LA (2 OF 5)  Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System Amended 11/6/2006 0:00
SA01944CH (1 OF 2) Modify airplane to fly on unleaded automotive gasoline 87 minimum antiknock index per ASTM Specification D-439 or D-4818 of any volatility class A through E or 82UL AVGAS per ASTM D-6227. Issued 3/5/2004
SA01951NY-D Installation of Wulfsberg P-2000 and/or C-2000-RT-2000 transceiver system. Reissued 3/18/2005
SA01988SE (PAGE 3) Installation of Electronics International Inc. Glass Panel Engine Monitor (with In-Flight Data) MVP-50P.  Issued 4/17/2009 0:00
SA02013CH Installation of a Royal International Model 9900BX Traffic Advisory System (TAS). Amended 5/2/2011
SA02015SE-D Installation of Garmin G500 Primary Flight Display (PFD) and Multifunction Display (MFD) System. Amended 2/5/2014
SA02019SE-D Installation of Garmin GTN 6XX/7XX Navigation System Amended 12/13/2013
SA02033AT (PAGE 2) Modification to install an air-oil separator to prevent oil from being aspirated from the engine breather line (47J series w stc s SH4-235SW SH4-826SW or SH479SW) Amended 7/25/2008
SA02049SE Fabrication of Stene Aviation Inc. Wing Tip Part Numbers SA-0523565-29 and SA-0523565-30 Issued 2/2/2010
SA02069AK Fabrication and Installation of the Airglas PA32-206LA Nose Fork equipped with Goodyear 8.50 x 6 tires. Amended 6/5/2006
SA02072AK Installation of hourmeter airspeed switch. Amended 11/14/1997
SA02110CH (PAGE 1) Installation of a Time Trac Data Recorder  Reissued 1/11/2010
SA02119SE Page 1 Installation of Garmin GDL 88 ADS-B UAT Transceiver System Issued 12/28/2012
SA02138AT Installation of Lord Corporation nose wheel shimmy damper part number SE-1051-2/3. Amended 8/11/2006
SA02149AK Installation of GX50/60 GPS Navigator Capstone configured MX20 Multi-Function Display and UAT transceiver. Reissued 5/17/2013
SA02153LA-D (Page 1) Installation of Garmin G600 Primary Flight Display (PFD) and Multifunction Display (MFD) System Amended 12/16/2013
SA02154AK (PAGE 1 ) Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display P/N 430-0270-500. Amended 1/12/2005
SA02155AK Installation of Hartzell model HC-C2YR-1BF/F8477-4 propeller and Hartzell model C-1576 damper assembly. Reissued 1/15/2004
SA02186AK Installation of Hartzell HC-C2YR-1BF/F8477-4 or HC-C2YK-1BF/F8477-4 propeller and Hartzell model C1576 damper assembly. Reissued 6/16/2004
SA02203AK (PAGE 1) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Amended 12/21/2011
SA02211CH Installation of a Three Point Torso Restraint System  Issued 11/15/2005
SA02212AK (PG 1) Replacement of existing landing and/or taxi light reflector and bulbs with high intensity discharge (HID) lighting systems  Amended 5/4/2011
SA02217AK (2 OF 5) Installation of Garmin AT Model GDL90 UAT Data Link System in accordance with Garmin AT Inc. GDL 90 UAT Master Data List P/N 560-0278-01 Revision A dated November 12 2004 or later FAA approved revision.  Amended 12/1/2004 0:00
SA02231AK Installation of Cleveland Main Wheels and Brakes. Reissued 3/17/2008
SA02245CH Installation of a MT-Propeller model MTV-15-() propeller and P-237-12 or P-277-B spinner assembly  Amended 5/1/2008
SA02246LA Installation of a flap handle extension. Amended 11/16/2010
SA02262SE Installation of split seam wing strut cuff as replacement parts for the strut fairings Issued 3/8/2013
SA02265SE Installation of a camera housing Amended 11/1/2013
SA02268CH (PAGE 1) Installation of Airwolf Filter Corp. Air Oil Separator Amended 8/28/2011
SA02276AK Installation of AMSAFE Aviation Inflatable Restraints Amended 3/12/2013
SA02282AK Installation of Lycoming IO-360 (200 or 180 hp) engine and associated powerplant components including propeller modified exhaust baffling cowling modifications. Amended 4/19/2010
SA02283SE Page 1 Installation of Electronics International Inc. Glass Panel Engine Monitor (with In Flight Data) CGR-30P Reissued 8/27/2013
SA02293AK (1 OF 3) Installation of FlightLogic Synthetic Vision Electronic Flight Information System (EFIS-SV). Reissued 1/11/2010
SA02332AK Installation of a fixed mounted Forward.Vision Enhanced Vision System (EVS) Models 100/600 to include an under-wing conformal fairing with sensor and a glareshield mounted dedicated display monitor Issued 6/24/2009
SA02343AK Installation of Lycoming Engine Model IO-390-A1A6 or IO-390-A3A6 Hartzell model HC-C2YR-1BFP/F8477-4 or MT propeller model MTV-15-B/210-58 Issued 6/22/2010
SA02359AK-D Fabrication and installation of F. Atlee dodge Aircraft Services Cessna Tie-Down clamp  Issued 11/6/2009
SA02376AK Replacement of tricycle landing gear with conventional (tail-wheel) landing gear Issued 12/12/2010
SA02386AT Installation of engine cowling and firewall fasteners. Issued 8/29/2001
SA02411CH Installation of the Aero Vent Cabin Ventilation System. Issued 7/25/2008
SA02415CH Installation of Flight Boss LTD S-RPE-CN Rudder Pedal Extensions. Issued 5/10/2007
SA02434NY Installation of a Digital Engine Monitoring system. Amended 2/7/2012
SA02446CH Installation of the Courtesy Light Kit. Issued 6/25/2007
SA02462CH Installation of Flight Boss LTD S-RPE-CO Rudder Pedal Extensions Issued 8/29/2007
SA02520AT Installation of M-20 Oil Separator model 600-WP. Issued 5/30/2002
SA02547AT (PG 1) Installation of a Voice Alert System. Amended 8/28/2007
SA02648AT Installation of Lycoming model O-360-A4M engine McCauley model 1A200/DFA8242 propeller two oil coolers engine exhaust system four NACA scoops for cabin and oil cooler ram air and a triple banner tow/release mechanism. Limited to installation on Cessna 175 serial number 55238 ONLY. Issued 4/1/2003
SA02655AT (1 OF 2) Installation of JAARS Model F5K Automatic Flight Following System (AFFS) in Helio H-295 type aircraft. Amended 9/1/2004
SA02717NY Installation of VoiceFlight Systems LLC VFS101 Speech Recognition Module Amended 1/9/2012
SA02738CH (PAGE 4) Installation of L-3 Communications Avionics Systems Amended 5/7/2010
SA02795AT Installation of a PXE7300SR In-Flight Entertainment System Issued 2/12/2004
SA02930NY Installation of Insight Instrument Corporation Graphic Engine Monitor (GEM 610C) models G3 G2 and G1 as primary Cylinder Head Temperature (CHT) Exhaust Gas Temperature (EGT) and Turbine Inlet Temperature (TIT) Instruments. Reissued 6/12/2012
SA02987CH Installation of the Electroair Electronic Ignition System Amended 7/23/2013
SA03148NY ( PAGE 1 OF 2) The installation of the Latitude Technologies Corporation S100 Tracking System Issued 9/26/2012
SA09133AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-612 with optional autotrim. Amended 2/28/2001
SA09149AC-D Installation of S-TEC System 55 two axis automatic flight guidance system Model ST-627 with optional autotrim system. Amended 2/20/2001
SA09149SC Modification of nose gear fork P/N SK150-11 to the SK182-34 configuration. Amended 2/22/1996
SA09154AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-616 with Optional Autotrim System. Amended 10/12/2001
SA09157AC-D Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System Model ST-633 with Optional Autotrim System. Amended 10/18/2001
SA09161AC-D Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems Model ST-182-40/50. Issued 8/7/1996
SA09209AC-D Installation of S-TEC System 20/30 single and two axis automatic flight guidance systems Model ST-671-20/30. Amended 8/27/1999
SA09215AC-D Installation of S-TEC System 30 ALT altitude hold system Model ST-673. Issued 5/16/1997
SA09225AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems. Issued 5/23/1997
SA09229AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-686. Issued 6/4/1997
SA09238AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-674-20/30. Issued 6/16/1997
SA09279AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-675. Issued 10/10/1997
SA09427AC-D Installation of S-TEC System 40X/50X Single and Two Axis Automatic Flight Guidance Systems Model ST-868-40X/50X. Issued 3/17/2000
SA09442AC-D Installation of S-TEC System 20/30 Single and Two Axis Automatic Flight Guidance Systems Model ST-874-20/30. Issued 7/24/2000
SA09445AC-D Installation of S-TEC System 30 ALT Altitude Hold System Model ST-875. Issued 5/1/2000
SA09470SC Installation of Starter Indicator light system. Issued 6/18/2001
SA1-124 Lube oil filter BP55-1. Issued 
SA1-219 Gyro-stabilizer 69A122. Issued 
SA1-252 Safety gear Model A. Issued 
SA1-426 Auxiliary seat in baggage compartment. Reissued 10/25/2001
SA1-516 Griswold lateralizer and heading lock. Amended 
SA1-545 External electrical power receptacle. Reissued 10/15/1974
SA1-610 Wet-to-dry vacuum pump conversion kit 300-2. Reissued 4/22/2003
SA1-612 Installation of Tactair T-101 autopilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). Reissued 8/7/1972
SA10005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Reissued 12/29/2006
SA1005SC Installation of airflow register into baggage compartment cover and insert a screened vent into empennage inspection plate. Issued 7/23/2002
SA10077SC Installation of push-button starter system. Amended 4/26/2005
SA10126SC (1 OF 2) Installation of Aero Advantage ADV200 series vacuum pump per Aero Advantage Drawing Number ADVMSI 500 latest FAA approved revision.  Amended 10/23/2003
SA1017NE Installation of .187 in thick windshield. Issued 10/16/1992
SA10236SC (2 OF 4) Installation of a GDC 31 Roll Steering Converter  Amended 3/22/2011
SA10822SC Installation of EFD1000 Primary Flight Display Amended 9/29/2009
SA1087GL Installation of a Shadin Co. fuel flow indicating system. Reissued 6/8/2006
SA109SW Automatic pilot AK106. Issued 1/1/1961
SA10WE Arens Vernier type throttle control. Issued 1/1/1961
SA11137SC Installation of Plane-Power ALT-FLX alternator Reissued 5/10/2013
SA1117NW Installation of an 18 inch diameter camera hole in the rear passenger area floor and an optical scanner mounted in the left pilot s window Issued 1/16/1981
SA115NW Modification of R.H. Door and the addition of a jump seat. Amended 4/30/1981
SA1168SO Installation of Aqua Model 2200 floats. Amended 8/15/2001
SA1177WE WECO carburetor temperature monitor. Issued 1/1/1960
SA11SO Tank type end plates. Issued 1/1/1960
SA1210GL Install SAT-T-STOP auxiliary seat stop device. Reissued 6/15/2012
SA121CE Nose and main gear wheel fairing(Jetstreams) using standard unaltered Cessna landing gear and nose gear fork for model and year using 500 x 5 nose and 600 x 6 main gear tires. Amended 3/1/1977
SA122NW Installation of a Continental O-470 series engine McCauley propeller engine mount cowling baffles and associated parts on the Cessna 175 and P172D series aircraft Reissued 10/24/2012
SA1261WE Installation of control position indicator (CPI) system. Reissued 2/18/1972
SA1295SO Installation of an adjustable nine-inch trim tab on left aileron. Issued 11/13/1981
SA12CE Removal of right cabin door. Issued 2/25/1962
SA12WE Installation of fiberglass wing tips. Reissued 5/4/2010
SA1315WE Installation of Mixture Monitor (exhaust gas temperature probe gage and selector) in accordance with Delta Products Part Lists A-192 and A-193 or in accordance with Tri-Star Corporation Mixture Monitor Installation Instructions dated December 9 1981 or later FAA approved revision and/or Drawing List MM-127 dated November 15 1981 or later FAA approved revision in aircraft models listed in Master Eligibility List P-80-A-6 revised March 29 1968 copy attached or later FAA approved revision. Reissued 4/15/2011
SA1371SW Wing leading cuff wing tips and upper surface flow fences. Amended 4/14/1983
SA1399SO Remove drain plug Cessna P/N MS20913-1 or MS20913-1D from bottom of fuel selector valve body and replace with drain valve Middle Tennessee P/N MT-1075. (175 S/N 28700A 55001-56238) (175A 619 56239-56777) (175B 17556778-17557002) (175C 17557003-17557119 ) Amended 2/17/2004
SA13GL Installation of Cleveland wheel No. 40-97A and brake No. 30-63A. (140A S/N 13400 AND UP) Amended 4/1/1981
SA1418SO Replacement of rotor vanes in Airborne 211CC and 212CW vacuum pumps. (See limitations) Reissued 6/12/1984
SA1431WE Installation of rudder trim system. Amended 4/2/1978
SA1437CE Continental IO-360-K or KB engine installation rerated to 210 hp (2800 rpm) at takeoff and 195 hp(2600 rpm) maximum continuous. Rerated engine designation IO-360-KC/STC SE1436CE or IO-360-KBC/STC SE1436CE. (R172K LANDPLANE AND FLOATPLANE) Reissued 4/7/2008
SA1455NM Installation of a flame proof auxiliary heater-dryer Model12-1600. Amended 12/11/1985
SA1455WE Installation of Brittain Industries Model CSA-1 Flight Control System Amended 9/12/1979
SA1473WE Installation of Brittain Model B2C Flight Control System. Reissued 10/20/1972
SA1474SW Installation of MASA 1223000-7 and -8 wing tip. Reissued 9/5/1979
SA147CE Moni-Meters on aircraft equipped with King KY-90 KY-95 Narco Mark 4 or Mark 12 transceivers. Issued 1/1/1960
SA1491CE Installation of flap and aileron gap seals. Amended 2/24/2005
SA1492CE Installation of flap and aileron gap seals. Reissued 1/27/1993
SA1500GL Installation of on-board engine analyzer system. Issued 7/18/1990
SA150NW Installation of flap gap seals. Amended 3/22/1994
SA1512WE (1 OF 2) Installation of exhaust gas temperature monitoring systems Model EGT-1. Amended 2/22/2007
SA1518GL Install shoulder harness and seat belt assembly. Issued 8/31/1990
SA1568CE-D Installation of KAP 100 single axis KAP 150 two axis or KFC 150 two axis flight control system. Reissued 2/28/2000
SA156NW Installation of baggage hatch with cover on EDO Model 2200 floats Issued 7/15/1975
SA157NE Installation of Graphic Engine Monitor System Model GEM-602 S/N 403 and GEM-603 S/N001126and subsequent. Amended 10/18/1996
SA1588WE Installation of supplemental exterior flashing lights. Issued 1/30/1968
SA158CE Cessna wing tips and attached lights 1223000-1 left 1223000-2 right tips and 1423006-12 left 0423006-13 right lights or an eqivalent. Issued 1/1/1960
SA1614WE Installation of one 12-gallon auxiliary fuel tank in each outboard wing panel. Amended 12/6/2006
SA1626NM Page 1 Installation of Electronics Int l Digital EGT/CHT Instruments and accessories. (201 Series) Amended 3/9/1993
SA1643GL Installation of V-type or Y-type shoulder harness. (182 SERIES EXCEPT R182 & TR182) Amended 8/31/1995
SA1668CE Installation strut/wing and strut/fuselage fairings lightning hole covers and aerodynamic putty. Reissued 1/27/1993
SA1686WE Installation of Vibration Isolation Products (VIP) engine mount P/Ns VIP 50525-1 and VIP 50545-1 on various aircraft as shown on FAA Approved Model List (AML) No. SA1686WE. Amended 10/17/2002
SA170CH Install a control yoke and instrument panel. Amended 7/1/2009
SA175EA Installation of wing struts modified to include Wings With Springs Model200 hydraulic-pneumatic shock absorbers and associated airframe modifications. Amended 8/17/1977
SA1760SO Installation of Appalachian Access. stainless steel brake rotors P/N 75-15C. Reissued 2/6/1995
SA179NW Installation of flap gap seals Issued 11/25/1975
SA17EA Installation of Tactair T-101 auto- pilot and optional installation of Tactair T-201 autopilot accessory kit (for use with Tactair T-101 autopilot). Reissued 8/7/1972
SA1824NM Installation of Lompoc Aero Specialties inner plexiglass pane );INSERT INTO stc_table VALUES ( in swing out window frames presently employing a single window - in accordance with Lompoc Aero Specialties FAA sealed Eligibility List dated January 4 1983 together with their FAA sealed Installation Instructions dated September 20 1982 or later FAA approved revisions. Manufacturer of the windows is controlled by Lompoc Aero Specialties drawings LAS 1012 dated August 6 1982 LAS 1013 dated October 5 1982 and LAS 1014 dated October 6 1982 or later FAA approved sealed revisions.I Reissued 1/23/2004
SA1827CE Installation of photo bubble in baggage door opening. Reissued 2/16/1983
SA182CH Installation of removable Telonics telemetry antennas. Reissued 5/4/1994
SA1895NM Installation of flap gas fairing. Issued 8/1/1983
SA2-1178 Replacement of right front seat with stretcher. Amended 11/14/2001
SA2-1533 Installation of windshield wiper. Reissued 1/31/1997
SA2067NM Installation of BAS Inc. TSO Shoulder Harness and BAS Inc. Harness System Amended 7/11/2012
SA20NW Installation of a Lycoming O-360-A1A engine and a Hartzell propeller Issued 12/29/1972
SA2105WE Installation of Model EGT-3 exhaust gas temperature monitor(with rising temperature alarm). (DC-6B (NAVY R6D-1Z) 680) Issued 2/9/1970
SA212GL Installation of windshield P/Ns W-2056 W/T-2056 or W/G-2056. Reissued 1/31/2007
SA2137SO Fabrication and installation of nose wheel fairings. Reissued 7/17/1989
SA2138CE Operation of airplane on unleaded automotive gasoline 87 minimum antiknock index and leaded automotive gasoline 88 minimum antiknock index (RON+MON)/2. Amended 6/23/1992
SA2162NM Installation of the Precise Flight stand-by vacuum system (SVS) Amended 11/7/2003
SA2190NM Page 1 Installation of electronics International Digital Volt/Amp Gauges and Accessories. Issued 2/16/1984
SA2190SO Replacement of Cleveland brake discs P/N 164-40 or 164-140 with Appalachian Accessories stainless steel brake discs P/N 75-40. Reissued 2/6/1995
SA220SO Tow bar release mechanism and safety tow link. Reissued 10/3/2011
SA221SO To remove right door for hauling sky divers picture making and etc. Reissued 1/2/2013
SA2229WE Installation of Madras wing tips Amended 2/21/1973
SA2256WE Installation of leading edge cuff on each wing. Reissued 1/21/2010
SA2282CE Installation of aileron and/or flap gap seals. Amended 10/10/1991
SA2298SO Replacement of Cleveland brake discs P/N 164-26A or 164-126A with Appalachian Accessories stainless steel brake discs P/N 75-27. Issued 4/18/1988
SA232EA Installation of Tactair omni lock model OL-1 and optional installation of Tactair localizer adapter model LA-1 (for use with Tactair model omni lock model OL-1). Reissued 8/7/1972
SA2350NM Page 1 Installation of Electronics International Inc digital carburetor/outside air temperature gauges Amended 6/6/1990
SA2381NM Installation of Knots 2U Ltd Wheel and Body Fairings Amended 8/19/2008
SA2381SO Installation of Appalachian Accessories P/N 75-92 Brake Rotors. (182 SERIES THRU 182A) Reissued 9/29/1995
SA2382NM Installation of Aileron and Flap Gap Seals. Amended 7/15/2003
SA2382SO Installation of Appalachian Accessories stainless steel brake discs. (182 SERIES THRU 182Q) Reissued 9/29/1995
SA2383SO Installation of Appalachian Accessories P/N 75-94 Brake Rotors. Reissued 9/29/1995
SA238SW Installation of cargo door. Reissued 3/9/1987
SA2518CE Installation of replacement wing tips. Amended 11/4/1992
SA2557NM (1 OF 2) Installation of KS Avionics EGT/CHT-2( ) combined exhaust gas and cylinder head temperature monitoring system. Amended 2/22/2007
SA256NW Installation of aileron gap seals.  Amended 4/12/1993
SA2586NM (PAGE 2) Installation of J.P. Instruments temperature monitoring systems. Amended 7/20/2008 0:00
SA2682CE Installation of steering rod boots. Issued 12/19/1990
SA2687NM (PAGE 1) Installation of Truboplus/ Electronics Int l gauges and switches. Amended 10/25/2000
SA2693NM (PAGE 1) Installation of Electronics International digital volt/amp gauges and accessories. Amended 12/10/2009
SA2710WE Installation of carburetor heat box bearings. Issued 6/15/1973
SA2792CE Installation of wing mounted convex mirror for inspection of nose and main landing gear position. Issued 2/6/1992
SA2844CE (1 OF 2) Installation of a plastic cap enclosure over the anti-collision strobe light system. Issued 7/29/1992
SA2853SW Leading edge cuffs stall fences aileron seals wing tips. Amended 3/2/1989
SA28WE Federal F-300 autopilot. Issued 1/1/1960
SA293NW Installation of Franklin 6A-350-C1 or 6A-350-C2 engines Hartzell HC-C2YF-1BF/F8459A -4 to -8 HC-C2YF-1BF/F8459A-4Q to -8Q or McCauley 2A31C21/84S-4 to -8 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 SF20821 or SF 20820 on Cessna Models 170A 170B 172 172A 172B through P 175 175A 175B and 175C as defined in AML. );INSERT INTO stc_table VALUES ( 2.) Installation of Franklin 6A-350-C1R engines Hartzell HC-C2YF-1BF/F8459A-4 to -8 HC-C2YF-1BF/F8459-4Q to -8 McCauley 2A31C21/84S-4 to -8 or 2A34C201/90DA-10 to -14 propellers in accordance with Seaplane Flying Inc. Assembly and Installation Instructions SF 20690 on Cessna Models 170A 170B (Serial Numbers 20267 to 26504) as defined in AML. Amended 4/21/2011
SA2960NM Install stay put (seat position locking device). Amended 3/14/1986
SA3-285 18-gallon auxiliary fuel system. Issued 1/1/1960
SA3-333 Installation of Doyn fiberglass wheel fairings. Reissued 8/16/2011
SA3-576 Installation of speed kit. Reissued 1/27/1993
SA3-611 Model 3000 main ski and Model 2000 nose ski. Issued 1/1/1960
SA3-674 Installation of Lycoming O-360-A1D engine and McCauley 2D36C14/78KM-4 or Hartzell HC-C2YK-1A/7666-2 propeller in accordance with Doyn Aircraft Drawing List for Model 1700 conversion dated May 6 1964 for Cessna Model 175B: Atlas Aviation Oil Cooler Installation dated September 12 1967 is required. Reissued 7/14/2011
SA3-691 Installation of Doyn swept-tail assembly kit 1400. Reissued 8/16/2011
SA300CE Installation of Woodward propeller governors on single and twin engine aircraft. (PA-31-325 modified per Colemill STC SA 970SO) Amended 5/14/1992
SA308EA (1 OF 2) Installation of carburetor ice detection system 105AP in single and twin engine aircraft and single engine helicopters powered by Continental Franklin and Lycoming type engines equipped with Marvel-Schebler MA-2 MA-3 MA-4 MA-4-5 MA-6 and HA-6 series carburetors. (Normal Utility and Acrobatic Category airplanes and helicopters equipped with engines and carburetors as described.) Amended 11/20/1978
SA3147SO Installation of aileron and flap gap seals. Reissued 1/23/2012
SA3203SO Replacement of Cleveland brake disks P/N 164-26A and/or 164-126A with Appalachian Accessories stainless steel brake disks P/N 75-27. Reissued 9/29/1995
SA3227SW-D Mitchell automatic flight system AK699 consisting of Century I autopilot with optional omni tracker. Reissued 12/7/1983
SA3228SW-D Mitchell automatic flight system AK698 consisting of Century IIB autopilot with optional radio coupler. Reissued 12/7/1983
SA327GL Installation of fuel tank caps. Issued 7/16/1979
SA3284SW-D Installation of Mitchell automatic flight system Model AK730 consisting of a Century I autopilot with optional omni tracking system. Reissued 3/28/1984
SA3285SO Installation of engine cowling and firewall fasteners. (172 S/N 54893 THRU 76673) (R172 SERIES S/N 2000 THRU 3454) Amended 8/29/2001
SA3285SW-D Mitchell automatic flight system AK731 consisting of Century IIB autopilot with optional radio coupler. Reissued 3/29/1984
SA3286SW-D Mitchell automatic flight system AK732 consisting of Century III autopilot with optional radio and glide slope couplers. Reissued 3/29/1984
SA3363SW Mitchell automatic flight system AK861 consisting of Century 21 autopilot. Reissued 3/24/1983
SA3487WE Installation of tail flood light. Reissued 2/28/1980
SA3531NM Installing copper electrical cables. (182 S/N 33000 THRU 33842) (8E 833 and UP) Reissued 9/8/2010
SA356CH Installation of seaplane safety covers. Issued 5/22/1995
SA3585NM Installation of ARNAV Systems FC-10 or FT-10 digital fuel flow indicating system. Issued 4/3/1987
SA3691NM Cockpit sunvisor installation Reissued 3/24/2003
Fusulage Construction
Airframe Material
Number of Doors
Wing Location
Wing Construction
Wing Rib Material
Wing Skin Material
Aileron Type
Aileron Trim
Aileron Control System
Flap Type
Wing Flap Actuation
Empennage Type
Empennage Rib Material
Empennage Skin Material
Rudder Trim
Yaw Trim Actuator
Yaw Control System
Pitch Trim
Pitch Control System
Pitch Trim Actuator
Landing Gear
Landing Gear Type
Retraction System
Emergency Extension
Ground Steering
Shock Absorbtion Main Gear
Shock Absorbtion Other Gear
Brake Type
Brake Controls
Instrument Panel
Flight Control
Number of Seats
Window Defrost
Normal Climb Profile Speed (KIAS)
Maximum Climb Profile Speed (KIAS)
Number of Engines
Engine Manufacturer
Engine Model
Engine Type
Fuel/Air Mechanism
Number of Cylinders
Max HP
Starter System
Propeller Manufacturer
Propeller Model
Number of Blades
Minimum Diameter
Maximum Diameter
Propeller Type
Propeller Governor
Fuel System
Fuel System Type
Approved Fuel Type 1
Approved Fuel Type 2
Approved Fuel Type 3
Fuel Capacity (G)
Tank Type 1 Location
Tank Type 1 Capacity (G)
Tank Type 2 Location
Tank Type 2 Capacity (G)
Usable Fuel (G)
Oil Capacity (Quarts)
Electrical System
Power Source
Power Storage
System Voltage
Alternator Amp
Battery Voltage
Battery Amp/Hour
Maximum T/O Weight (lbs)
Maximum LDG Weight (lbs)
Standard Empty Weight (lbs)
Useful Load (lbs) 0
Station 1 Baggage Location
Max Weight Station 1 (lbs)
Station 2 Baggage Location
Max Weight Station 2(lbs)
Station 3 Baggage Location
Max Weight Station 3(lbs)
Wing Loading (lbs/sq.ft)
Vne (KCAS)
Vno (KCAS)
Va(Max Gross) (KCAS)


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